Date:
November 16th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6727 44 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 1218)
---------------------------------------
Vector Time (GMT): 2008/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -850197
50 A = 6727383
51 meter
Y = 4938178
11 meter E =
0010376
Z = 4486450
85 I = 51
44457
XDOT = -6826
054614 Wp = 44
33038
YDOT = 1685
566550 meter/sec RA = 325
29807 deg
ZDOT = -3137
168865 TA = 77
13043
MA = 77
01453
Ha = 192
464 n
mi
Hp = 186
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2789361
87 X = -927148
86
Y = 16201371
76 feet Y = 4928239
93 meter
Z = 14719326
92 Z = 4482134
11
XDOT = -22395
192303 XDOT = -6829
155287
YDOT = 5530
073984 feet/sec YDOT = 1609
216694 meter/sec
ZDOT = -10292
548770 ZDOT = -3170
338211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11252340
88 X = -3429713
50
Y = -12005501
08 feet Y = -3659276
73 meter
Z = 14702936
44 Z = 4481455
03
XDOT = 8074
763078 XDOT = 2461
187786
YDOT = -20377
565433 feet/sec YDOT = -6211
081944 meter/sec
ZDOT = -10420
993662 ZDOT = -3176
318868
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08319
54208022
00020000 00000-0 20000-3 0 9003
2 25544 51
6411 325
6449 0004071 346
4237 13
6815 15
72621174 12197
Satellite: ISS
Catalog Number: 25544
Epoch time: 08319
54208022 = yrday
fracday
Element set: 900
Inclination: 51
6411 deg
RA of node: 325
6449 deg
Eccentricity:
0004071
Arg of perigee: 346
4237 deg
Mean anomaly: 13
6815 deg
Mean motion: 15
72621174 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1219
Checksum: 262
Coasting Arc #2 (Orbit 1234)
---------------------------------------
Vector Time (GMT): 2008/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5821316
99 A = 6733594
31 meter
Y = -2411987
91 meter E =
0014870
Z = 2349592
36 I = 51
44230
XDOT = 99
944481 Wp = 57
76404
YDOT = 5505
735358 meter/sec RA = 320
20356 deg
ZDOT = 5387
347840 TA = 328
77381
MA = 328
86206
Ha = 192
408 n
mi
Hp = 185
994
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19098809
02 X = 5836441
40
Y = -7913346
16 feet Y = -2346806
32 meter
Z = 7708636
36 Z = 2377909
43
XDOT = 327
901840 XDOT = 12
199636
YDOT = 18063
436214 feet/sec YDOT = 5506
361693 meter/sec
ZDOT = 17675
025723 ZDOT = 5387
620955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4731482
29 X = -1442155
80
Y = 20082254
52 feet Y = 6121071
18 meter
Z = 7818232
30 Z = 2382997
21
XDOT = -13316
812333 XDOT = -4058
964399
YDOT = -10040
521084 feet/sec YDOT = -3060
350826 meter/sec
ZDOT = 17676
463135 ZDOT = 5387
785964
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08320
55881000
00020000 00000-0 20000-3 0 9010
2 25544 51
6410 320
4346 0004062 349
5218 10
5859 15
72639347 12351
Satellite: ISS
Catalog Number: 25544
Epoch time: 08320
55881000 = yrday
fracday
Element set: 901
Inclination: 51
6410 deg
RA of node: 320
4346 deg
Eccentricity:
0004062
Arg of perigee: 349
5218 deg
Mean anomaly: 10
5859 deg
Mean motion: 15
72639347 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1235
Checksum: 263
Coasting Arc #3 (Orbit 1249)
---------------------------------------
Vector Time (GMT): 2008/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -982718
38 A = 6725754
21 meter
Y = -4529792
17 meter E =
0011369
Z = -4883034
13 I = 51
39362
XDOT = 6312
408079 Wp = 86
54520
YDOT = -3778
694890 meter/sec RA = 315
02356 deg
ZDOT = 2240
118706 TA = 205
31220
MA = 205
36794
Ha = 192
615 n
mi
Hp = 185
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3224141
67 X = -908271
17
Y = -14861522
86 feet Y = -4540364
63 meter
Z = -16020453
19 Z = -4887627
98
XDOT = 20710
000259 XDOT = 6343
310628
YDOT = -12397
292946 feet/sec YDOT = -3707
933387 meter/sec
ZDOT = 7349
470821 ZDOT = 2270
859511
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13988586
90 X = 4263721
29
Y = 5915947
39 feet Y = 1803180
76 meter
Z = -16038574
58 Z = -4888557
53
XDOT = -1194
337626 XDOT = -364
034109
YDOT = 23025
560827 feet/sec YDOT = 7018
190940 meter/sec
ZDOT = 7468
374812 ZDOT = 2276
360643
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08321
51198266
00020000 00000-0 20000-3 0 9023
2 25544 51
6408 315
5494 0004174 353
5498 6
5610 15
72617945 12503
Satellite: ISS
Catalog Number: 25544
Epoch time: 08321
51198266 = yrday
fracday
Element set: 902
Inclination: 51
6408 deg
RA of node: 315
5494 deg
Eccentricity:
0004174
Arg of perigee: 353
5498 deg
Mean anomaly: 6
5610 deg
Mean motion: 15
72617945 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1250
Checksum: 288
Coasting Arc #4 (Orbit 1265)
---------------------------------------
Vector Time (GMT): 2008/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5086815
90 A = 6734868
48 meter
Y = 4123189
86 meter E =
0005239
Z = -1573714
25 I = 51
40447
XDOT = -2039
895563 Wp = 113
99615
YDOT = -4700
513556 meter/sec RA = 309
91365 deg
ZDOT = -5738
970191 TA = 83
40075
MA = 83
34112
Ha = 192
687 n
mi
Hp = 185
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16689028
53 X = -5124899
10
Y = 13527525
80 feet Y = 4066093
38 meter
Z = -5163104
49 Z = -1598518
38
XDOT = -6692
570746 XDOT = -1959
302829
YDOT = -15421
632403 feet/sec YDOT = -4722
873633 meter/sec
ZDOT = -18828
642360 ZDOT = -5748
684853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1959032
63 X = -597113
15
Y = -21370087
99 feet Y = -6513602
82 meter
Z = -5258973
85 Z = -1602935
23
XDOT = 14917
633475 XDOT = 4546
894683
YDOT = 3261
791731 feet/sec YDOT = 994
194119 meter/sec
ZDOT = -18866
632876 ZDOT = -5750
549701
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08322
52868666
00020000 00000-0 20000-3 0 9034
2 25544 51
6403 310
3380 0004214 358
8639 1
2513 15
72662202 12662
Satellite: ISS
Catalog Number: 25544
Epoch time: 08322
52868666 = yrday
fracday
Element set: 903
Inclination: 51
6403 deg
RA of node: 310
3380 deg
Eccentricity:
0004214
Arg of perigee: 358
8639 deg
Mean anomaly: 1
2513 deg
Mean motion: 15
72662202 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1266
Checksum: 268
Coasting Arc #5 (Orbit 1281)
---------------------------------------
Vector Time (GMT): 2008/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2509830
87 A = 6724475
73 meter
Y = 3563747
37 meter E =
0007716
Z = 5118693
93 I = 51
35119
XDOT = -5156
680764 Wp = 27
78140
YDOT = 5560
964547 meter/sec RA = 304
74332 deg
ZDOT = -1335
668865 TA = 75
09310
MA = 75
00767
Ha = 192
653 n
mi
Hp = 185
634
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8234353
25 X = 2444927
99
Y = 11692084
55 feet Y = 3591450
45 meter
Z = 16793615
27 Z = 5130729
45
XDOT = -16918
243977 XDOT = -5211
992615
YDOT = 18244
634340 feet/sec YDOT = 5502
990403 meter/sec
ZDOT = -4382
115698 ZDOT = -1360
854184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14236862
06 X = -4339395
56
Y = 493189
77 feet Y = 150324
24 meter
Z = 16840530
00 Z = 5132993
54
XDOT = -6126
241832 XDOT = -1867
278510
YDOT = -23050
400593 feet/sec YDOT = -7025
762101 meter/sec
ZDOT = -4479
359802 ZDOT = -1365
308868
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08323
54537631
00020000 00000-0 20000-3 0 9043
2 25544 51
6398 305
1270 0004268
6826 359
4342 15
72682749 12828
Satellite: ISS
Catalog Number: 25544
Epoch time: 08323
54537631 = yrday
fracday
Element set: 904
Inclination: 51
6398 deg
RA of node: 305
1270 deg
Eccentricity:
0004268
Arg of perigee:
6826 deg
Mean anomaly: 359
4342 deg
Mean motion: 15
72682749 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1282
Checksum: 293
Coasting Arc #6 (Orbit 1297)
---------------------------------------
Vector Time (GMT): 2008/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3813657
34 A = 6735483
68 meter
Y = -5489090
01 meter E =
0016512
Z = 754175
84 I = 51
37308
XDOT = 3586
748328 Wp = 42
47728
YDOT = 3318
902195 meter/sec RA = 299
61750 deg
ZDOT = 5954
935156 TA = 325
77446
MA = 325
88077
Ha = 192
637 n
mi
Hp = 185
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12511999
14 X = 3871090
11
Y = -18008825
48 feet Y = -5446122
40 meter
Z = 2474330
20 Z = 772841
98
XDOT = 11767
547008 XDOT = 3520
440947
YDOT = 10888
786728 feet/sec YDOT = 3358
640209 meter/sec
ZDOT = 19537
188831 ZDOT = 5972
198886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8695929
62 X = 2650519
35
Y = 20121813
80 feet Y = 6133128
85 meter
Z = 2546300
23 Z = 776112
31
XDOT = -13933
829015 XDOT = -4247
031084
YDOT = 3515
177192 feet/sec YDOT = 1071
426008 meter/sec
ZDOT = 19604
361450 ZDOT = 5975
409370
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08324
56205070
00020000 00000-0 20000-3 0 9056
2 25544 51
6397 299
9166 0004084 5
7993 354
3216 15
72751227 12987
Satellite: ISS
Catalog Number: 25544
Epoch time: 08324
56205070 = yrday
fracday
Element set: 905
Inclination: 51
6397 deg
RA of node: 299
9166 deg
Eccentricity:
0004084
Arg of perigee: 5
7993 deg
Mean anomaly: 354
3216 deg
Mean motion: 15
72751227 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1298
Checksum: 305
Coasting Arc #7 (Orbit 1312)
---------------------------------------
Vector Time (GMT): 2008/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3630997
87 A = 6723842
11 meter
Y = -2158230
11 meter E =
0015955
Z = -5244652
60 I = 51
32007
XDOT = 3476
940104 Wp = 77
45331
YDOT = -6843
999559 meter/sec RA = 294
45918 deg
ZDOT = 413
682731 TA = 196
47333
MA = 196
52523
Ha = 192
835 n
mi
Hp = 185
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11912722
68 X = -3581116
42
Y = -7080807
45 feet Y = -2198554
92 meter
Z = -17206865
47 Z = -5262171
14
XDOT = 11407
283806 XDOT = 3551
202785
YDOT = -22454
066795 feet/sec YDOT = -6804
703196 meter/sec
ZDOT = 1357
226809 ZDOT = 430
754040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12140760
29 X = 3700503
74
Y = -6504246
86 feet Y = -1982494
44 meter
Z = -17274945
08 Z = -5265403
26
XDOT = 12945
201298 XDOT = 3945
697356
YDOT = 20423
029839 feet/sec YDOT = 6224
939495 meter/sec
ZDOT = 1422
908272 ZDOT = 433
702441
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08325
51517370
00020000 00000-0 20000-3 0 9062
2 25544 51
6397 295
0307 0004342 8
8633 351
2605 15
72711374 13138
Satellite: ISS
Catalog Number: 25544
Epoch time: 08325
51517370 = yrday
fracday
Element set: 906
Inclination: 51
6397 deg
RA of node: 295
0307 deg
Eccentricity:
0004342
Arg of perigee: 8
8633 deg
Mean anomaly: 351
2605 deg
Mean motion: 15
72711374 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1313
Checksum: 272
Coasting Arc #8 (Orbit 1328)
---------------------------------------
Vector Time (GMT): 2008/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2213167
57 A = 6735719
95 meter
Y = 6358675
35 meter E =
0010532
Z = 18234
03 I = 51
34979
XDOT = -4547
312174 Wp = 113
65763
YDOT = -1557
633140 meter/sec RA = 289
31479 deg
ZDOT = -6010
275925 TA = 66
14368
MA = 66
03334
Ha = 192
874 n
mi
Hp = 185
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7261048
47 X = -2284195
41
Y = 20861795
76 feet Y = 6333529
29 meter
Z = 59822
93 Z = 7309
95
XDOT = -14919
003196 XDOT = -4500
359170
YDOT = -5110
344947 feet/sec YDOT = -1608
221094 meter/sec
ZDOT = -19718
753035 ZDOT = -6032
253141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14466246
34 X = -4409311
88
Y = -16693361
58 feet Y = -5088136
61 meter
Z = 17944
15 Z = 5469
38
XDOT = 10592
801664 XDOT = 3228
685947
YDOT = -9233
038174 feet/sec YDOT = -2814
230035 meter/sec
ZDOT = -19804
076497 ZDOT = -6036
282516
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08326
53182225
00020000 00000-0 20000-3 0 9073
2 25544 51
6399 289
8191 0004457 11
8699 348
2568 15
72755533 13291
Satellite: ISS
Catalog Number: 25544
Epoch time: 08326
53182225 = yrday
fracday
Element set: 907
Inclination: 51
6399 deg
RA of node: 289
8191 deg
Eccentricity:
0004457
Arg of perigee: 11
8699 deg
Mean anomaly: 348
2568 deg
Mean motion: 15
72755533 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1329
Checksum: 326
Coasting Arc #9 (Orbit 1344)
---------------------------------------
Vector Time (GMT): 2008/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4190469
61 A = 6723660
59 meter
Y = 516273
02 meter E =
0004944
Z = 5229337
65 I = 51
30097
XDOT = -1513
497826 Wp = 47
17811
YDOT = 7537
646626 meter/sec RA = 284
17089 deg
ZDOT = 471
695481 TA = 38
33900
MA = 38
30386
Ha = 192
769 n
mi
Hp = 185
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13748259
89 X = 4158981
40
Y = 1693809
11 feet Y = 562957
03 meter
Z = 17156619
57 Z = 5249618
91
XDOT = -4965
544049 XDOT = -1599
963992
YDOT = 24729
811765 feet/sec YDOT = 7520
238344 meter/sec
ZDOT = 1547
557351 ZDOT = 464
132977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8081762
11 X = -2463321
09
Y = 11129380
59 feet Y = 3392235
20 meter
Z = 17235290
64 Z = 5253316
59
XDOT = -18431
263576 XDOT = -5617
849138
YDOT = -15720
844842 feet/sec YDOT = -4791
713508 meter/sec
ZDOT = 1518
803562 ZDOT = 462
931326
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08327
54845694
00020000 00000-0 20000-3 0 9082
2 25544 51
6401 284
6083 0004432 14
8148 345
3143 15
72774473 13452
Satellite: ISS
Catalog Number: 25544
Epoch time: 08327
54845694 = yrday
fracday
Element set: 908
Inclination: 51
6401 deg
RA of node: 284
6083 deg
Eccentricity:
0004432
Arg of perigee: 14
8148 deg
Mean anomaly: 345
3143 deg
Mean motion: 15
72774473 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1345
Checksum: 296
Coasting Arc #10 (Orbit 1359)
---------------------------------------
Vector Time (GMT): 2008/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 408168
22 A = 6735336
34 meter
Y = -6667673
05 meter E =
0014620
Z = -801105
99 I = 51
33435
XDOT = 4880
052636 Wp = 33
28465
YDOT = -407
787782 meter/sec RA = 279
00955 deg
ZDOT = 5943
739450 TA = 317
94371
MA = 318
05584
Ha = 192
922 n
mi
Hp = 184
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1339134
59 X = 486588
62
Y = -21875567
76 feet Y = -6662670
17 meter
Z = -2628300
50 Z = -798932
87
XDOT = 16010
671377 XDOT = 4855
375550
YDOT = -1337
886425 feet/sec YDOT = -353
354453 meter/sec
ZDOT = 19500
457513 ZDOT = 5967
387381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18694077
55 X = 5697954
84
Y = 11441450
70 feet Y = 3487354
17 meter
Z = -2620377
86 Z = -798691
17
XDOT = -5429
377943 XDOT = -1654
874397
YDOT = 13310
406330 feet/sec YDOT = 4057
011849 meter/sec
ZDOT = 19592
112840 ZDOT = 5971
675994
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08328
50153892
00020000 00000-0 20000-3 0 9092
2 25544 51
6399 279
7223 0004417 19
2446 340
8883 15
72792660 13608
Satellite: ISS
Catalog Number: 25544
Epoch time: 08328
50153892 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 279
7223 deg
Eccentricity:
0004417
Arg of perigee: 19
2446 deg
Mean anomaly: 340
8883 deg
Mean motion: 15
72792660 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1360
Checksum: 312
Coasting Arc #11 (Orbit 1375)
---------------------------------------
Vector Time (GMT): 2008/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4199139
72 A = 6724087
08 meter
Y = 1203265
84 meter E =
0016905
Z = -5126717
17 I = 51
29416
XDOT = -548
411342 Wp = 66
92949
YDOT = -7552
394222 meter/sec RA = 273
87848 deg
ZDOT = -1320
328576 TA = 190
33721
MA = 190
37201
Ha = 192
970 n
mi
Hp = 184
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13776705
12 X = -4187377
39
Y = 3947722
56 feet Y = 1156374
71 meter
Z = -16819938
23 Z = -5147088
51
XDOT = -1799
249810 XDOT = -457
504384
YDOT = -24778
196266 feet/sec YDOT = -7558
018505 meter/sec
ZDOT = -4331
786666 ZDOT = -1322
772482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2678606
83 X = 816439
36
Y = -13983811
61 feet Y = -4262265
78 meter
Z = -16898831
85 Z = -5150763
95
XDOT = 21873
472364 XDOT = 6667
034376
YDOT = 9448
900469 feet/sec YDOT = 2880
024863 meter/sec
ZDOT = -4341
831794 ZDOT = -1323
390331
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08329
51814609
00020000 00000-0 20000-3 0 9106
2 25544 51
6408 274
5104 0004449 21
9066 338
2286 15
72808577 13763
Satellite: ISS
Catalog Number: 25544
Epoch time: 08329
51814609 = yrday
fracday
Element set: 910
Inclination: 51
6408 deg
RA of node: 274
5104 deg
Eccentricity:
0004449
Arg of perigee: 21
9066 deg
Mean anomaly: 338
2286 deg
Mean motion: 15
72808577 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1376
Checksum: 301
Coasting Arc #12 (Orbit 1391)
---------------------------------------
Vector Time (GMT): 2008/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1343473
59 A = 6734530
53 meter
Y = 6422551
82 meter E =
0014591
Z = 1496656
69 I = 51
32949
XDOT = -4558
228487 Wp = 100
25945
YDOT = 2306
103367 meter/sec RA = 268
70326 deg
ZDOT = -5759
356228 TA = 63
19176
MA = 63
04260
Ha = 193
017 n
mi
Hp = 184
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4407721
75 X = 1264285
02
Y = 21071364
23 feet Y = 6437132
43 meter
Z = 4910290
96 Z = 1502991
64
XDOT = -14954
817870 XDOT = -4555
698224
YDOT = 7565
955928 feet/sec YDOT = 2255
145245 meter/sec
ZDOT = -18895
525684 ZDOT = -5781
494397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20862877
92 X = -6359005
19
Y = -5284328
36 feet Y = -1610663
28 meter
Z = 4935337
67 Z = 1504290
92
XDOT = -690
569918 XDOT = -210
485711
YDOT = -15138
558936 feet/sec YDOT = -4614
232764 meter/sec
ZDOT = -18981
190425 ZDOT = -5785
466842
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08330
53473940
00020000 00000-0 20000-3 0 9110
2 25544 51
6415 269
2990 0004485 26
1659 333
9729 15
72830111 13921
Satellite: ISS
Catalog Number: 25544
Epoch time: 08330
53473940 = yrday
fracday
Element set: 911
Inclination: 51
6415 deg
RA of node: 269
2990 deg
Eccentricity:
0004485
Arg of perigee: 26
1659 deg
Mean anomaly: 333
9729 deg
Mean motion: 15
72830111 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1392
Checksum: 293
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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